Overview
The Bell 212 is a twin-engine development of the Bell 205 family. Introduced in the late 1960s, it provided improved safety and performance. The aircraft remains widely used in civil and military roles.
Live Fleet Activity (B212)
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Specifications
Units
- Engine
- 1 × Pratt & Whitney Canada PT6T-3
- Engine type
- Turboshaft
- Power
- 1,800 shp · 1,342 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 15
- Crew
- —
- Cabin width
- 7 ft 10 in · 2.40 m
- Cabin height
- 3 ft 11 in · 1.20 m
- Cabin length
- 8 ft 10 in · 2.70 m
- Exterior length
- 57 ft 1 in · 17.40 m
- Tail height
- 12 ft 6 in · 3.80 m
- Fuselage diameter
- 8 ft 6 in · 2.60 m
- Wing span
- 47 ft 11 in · 14.60 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 11,200 lb · 5,100 kg
- Max landing weight
- —
- Max payload
- 4,700 lb · 2,150 kg
- Fuel capacity
- 300 gal · 1,100 L · 900 kg (Jet A)
- Max cruise speed
- 120 kt · 138 mph · 222 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 250 nm · 290 mi · 460 km
- Fuel burn
- —
- Ceiling
- 17,400 ft · 5,300 m
- Rate of climb
- 1,745 ft/min · 9 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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Live fleet activity details
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